C
We have recently switched our 1972 GE Frame 5 gas turbine from natural gas to liquid fuel only and cannot get it to light off. It is pre Atomising Air compressor model and was originally diesel only.
What I am looking for is a chart or graph relating rotor speed to compressor discharge pressure as we have looked at all the other components fuel, fuel pressure, fuel volume, spray pattern, fuel nozzle's replaced, ignitors checked, ignitors replaced time and again.
At crank (GT rotor at 850RPM) we get a maximum CDP of 5 kPa (0.72Psi) and I believe that's a bit low but cannot find any documentation to support this theory.
Thanks
Chris W
What I am looking for is a chart or graph relating rotor speed to compressor discharge pressure as we have looked at all the other components fuel, fuel pressure, fuel volume, spray pattern, fuel nozzle's replaced, ignitors checked, ignitors replaced time and again.
At crank (GT rotor at 850RPM) we get a maximum CDP of 5 kPa (0.72Psi) and I believe that's a bit low but cannot find any documentation to support this theory.
Thanks
Chris W